EP2347531A1 - Test par voie aérienne - Google Patents

Test par voie aérienne

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Publication number
EP2347531A1
EP2347531A1 EP09818841A EP09818841A EP2347531A1 EP 2347531 A1 EP2347531 A1 EP 2347531A1 EP 09818841 A EP09818841 A EP 09818841A EP 09818841 A EP09818841 A EP 09818841A EP 2347531 A1 EP2347531 A1 EP 2347531A1
Authority
EP
European Patent Office
Prior art keywords
antenna elements
antenna
emulator
ota
elements
Prior art date
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Application number
EP09818841A
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German (de)
English (en)
Other versions
EP2347531B1 (fr
EP2347531A4 (fr
Inventor
Pekka KYÖSTI
Jukka-Pekka Nuutinen
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Anite Telecoms Oy
Original Assignee
Elektrobit System Test Oy
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Publication of EP2347531A1 publication Critical patent/EP2347531A1/fr
Publication of EP2347531A4 publication Critical patent/EP2347531A4/fr
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Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q25/00—Antennas or antenna systems providing at least two radiating patterns
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B17/00—Monitoring; Testing
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R29/00—Arrangements for measuring or indicating electric quantities not covered by groups G01R19/00 - G01R27/00
    • G01R29/08—Measuring electromagnetic field characteristics
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/20—Arrays of individually energised antenna units similarly polarised and spaced apart the units being spaced along or adjacent to a curvilinear path
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B17/00—Monitoring; Testing
    • H04B17/30—Monitoring; Testing of propagation channels
    • H04B17/391—Modelling the propagation channel
    • H04B17/3912—Simulation models, e.g. distribution of spectral power density or received signal strength indicator [RSSI] for a given geographic region

Definitions

  • the invention relates to an over-the-air testing of a device in an an- echoic chamber.
  • a radio frequency signal When a radio frequency signal is transmitted from a transmitter to a receiver, the signal propagates in a radio channel along one or more paths having different angles of arrivals, signal delays and powers, which causes fadings of different durations and strengths in the received signal. In addition, noise and interference caused by other transmitters interfere with the radio connection.
  • a transmitter and a receiver can be tested using a radio channel emulator emulating real circumstances.
  • a channel is usually modeled with a FIR filter (Finite Impulse Response filter), which generates convolution between the channel model and an applied signal by weighting the signal, delayed by different delays, with channel coefficients, i.e. tap coefficients, and by summing the weighted signal components.
  • the channel coefficients are functions of time to correspond to the temporal behavior of a real channel.
  • a traditional radio channel emulator test is performed via a conducted connection such that a transmitter and a receiver are coupled together via a cable.
  • OTA Over The Air
  • the emulator which may be coupled to or act as a base station emulating paths between the subscriber terminal and the base station according to a channel model.
  • the direction of a path depends on the direction of an antenna, and hence the directions of paths are limited and there is a need for a better OTA test solution.
  • An object of the invention is to provide an improved solution.
  • a method of communicating with an electronic device under test through a simulated radio channel of an emulator comprises optimizing a cost function of a theoretical spatial cross correlation and a spatial correlation obtained with antenna elements for determining weights of the antenna elements; and forming, on the basis of the weights, a beam of a signal of at least one path of a simulated ra- dio channel with at least two antenna elements of a plurality of the antenna elements coupled to an emulator in an anechoic chamber.
  • a method of communicating with an electronic device under test through a simulated radio channel of an emulator comprises optimizing a cost function of a theoretical spatial cross correlation and a spatial correlation obtained with antenna elements for determining weights of the antenna elements; and forming, on the basis of the weights, a beam of a signal of at least one path of a simulated radio channel with at least two antenna elements of a plurality of the antenna elements coupled to an emulator in an anechoic chamber, the at least two antenna elements polarizing the beam in a known manner.
  • a testing system of communicating with an electronic device under test through a simulated radio channel of an emulator is configured to optimize a cost function of a theoretical spatial cross correlation and a spatial correlation obtained with antenna elements for determining weights of the antenna elements; and form, on the basis of the weights, a beam of a signal of at least one path of a simulated radio channel with at least two antenna elements of a plurality of the antenna elements coupled to an emulator in an anechoic chamber.
  • a testing system of communicating with an electronic device under test through a simulated radio channel of an emulator is provided.
  • the testing system is configured to optimize a cost function of a theoretical spatial cross correlation and a spatial correlation obtained with antenna elements for determining weights of the an- tenna elements; and form, on the basis of the weights, a beam of a signal of at least one path of a simulated radio channel with at least two antenna elements of a plurality of the antenna elements coupled to an emulator in an anechoic chamber, the at least two antenna elements being configured to polarize the beam in a known manner.
  • the invention provides several advantages. Spatial correlation characteristics and/or polarization characteristics can be taken into account in the weights of antenna elements.
  • Figure 1 illustrates a propagation of a radio signal
  • Figure 2 illustrates a power azimuth spectrum of reception beams
  • Figure 3 illustrates a power azimuth spectrum of transmission beams
  • Figure 4 shows a measurement configuration in an OTA test chamber
  • Figure 5 shows a beam to be modeled by the antenna elements
  • Figure 6 shows a group of antenna elements and associated an- tenna group switching network
  • Figure 7 shows a DUT surrounded by groups of antenna elements
  • Figure 8 presents controlling delays of antennas in a MIMO configuration
  • Figure 9 presents controlling delays of antennas in an OTA cham- ber
  • Figure 10 presents an AoA in an OTA chamber
  • Figure 11 presents antenna weighting of the antenna elements of Figure 10
  • Figure 12 presents spatial correlation of three antenna elements
  • Figure 13 presents weights of antenna elements and resulting PAS
  • Figure 14 presents a theoretical correlation and ideal spatial correlation
  • Figure 15 presents a PDP of six clusters
  • Figure 16 presents a delay tap mapping of eight channels
  • Figure 17 presents a situation where a DUT spatial resolution is narrower than a spacing of the antenna elements
  • Figure 18 presents a PAS in the situation of Figure 17
  • Figure 19 presents a situation where a DUT spatial resolution is wider than a spacing of the antenna elements
  • Figure 20 presents a PAS in the situation of Figure 19
  • Figure 21 presents a PAS of three and five antenna elements
  • Figure 22 presents polarizing antenna elements
  • Figure 23 shows a flow chart of a method of optimizing an l_ p -norm
  • Figure 24 shows a flow chart of a method of optimizing an L ⁇ norm with polarizing antenna elements.
  • FIG. 1 illustrates a propagation of a radio signal between a transmitter and a receiver.
  • the transmitter 100 may comprise an antenna 102 of at least one antenna element 104 to 110.
  • the antenna may be, for example, ULA (Uniform Linear Array) antenna where the spacing between the antenna elements is constant, for example half a wavelength of the radio signal.
  • the transmitter 100 may be a base station of a radio system.
  • the receiver 112 may comprise an antenna 114 of at least one antenna element 116 to 122.
  • the receiver 112 may be a subscriber terminal of a radio system.
  • a transmission beam 124 may be directed to an angle ⁇ i and its angle spread may be ⁇ ⁇ which may be x ⁇ f ⁇ , where x is a real number larger than zero and ⁇ is a standard deviation of the angle ⁇ i.
  • Each cluster 126, 128 may have a number of active regions 1260 to 1264, 1280 to 1284 which predominantly reflect and/scatter in the cluster 126, 128.
  • a cluster 126, 128 may be fixed or moving, and a cluster 126, 128 may be a natural or man-made object such as a building, a train, a mountain etc.
  • the active regions may be some finer structural features on an object.
  • the reflected and/or scattered beam may be directed towards the antenna 114 of the receiver 112.
  • the antenna 114 may have a reception angle ⁇ and its angle spread may be ⁇ ⁇ which may be y ⁇ S* td , where y is a real number larger than zero and ⁇ ⁇ is a standard deviation of angle ⁇ i.
  • the antenna 114 may also have a beam from a reception angle ⁇ 2 and its angle spread may be ⁇ ⁇ 2 .
  • the propagation from a transmitter 100 to a receiver 112 via at least one cluster 126, 128 causes an additional delay to a signal with respect to a signal traveling straight along a line-of-sight.
  • Clusters 126, 128 in a radio channel are responsible for multi path propagation. It can be approximated that a path and a cluster 126, 128 have a correspondence such that one received path comes from one cluster.
  • a radio channel may be described by cluster powers, delays, nominal AoA (Angle of Arrival) and AoD (Angle of Departure), and angle spreads of clusters at both arrival and departure ends.
  • information on the receiver and transmitter antenna arrays is required. The information may include values of parameters of an antenna array geometry and an antenna field pattern (beam). Also the subscriber terminal velocity vector and/or the cluster Doppler frequency component may be needed.
  • Table 1 presents an example of a clustered delay line model of a radio channel in an urban environment.
  • Clusters 1 and 3 have three active regions which have different delays and powers.
  • An ASD Angle Spread of Departure
  • ASD 2° in this example
  • an ASA Angle Spread of Arrival
  • XPR Cross Polarization Power ratio
  • XPR 7 dB in this example. They may also be different for different clusters.
  • An impulse response estimate H U]Sin (t, ⁇ ) of a radio channel may be expressed in a mathematical form as follows:
  • F tx,s is a transmission antenna field pattern (i.e. transmission beam)
  • F r ⁇ iU is a reception antenna field pattern (i.e. reception beam)
  • d s is a distance between the antenna elements in a ULA transmission antenna
  • d u is a distance between the antenna elements in a ULA reception antenna
  • P n means a cluster power
  • M means the number of active regions in a cluster
  • m is an index of an active region
  • n is an index of a cluster
  • ⁇ n m is a constant phase term of a scatterer n,m
  • o n ,m is a Doppler frequency of an active region having index n,m and ⁇ is a delay.
  • a Doppler frequency of an active region having index n,m can be expressed as: where v is a velocity vector and
  • the impulse response estimate in equation (1) may be simplified, when the receiver antenna is assumed omnidirectional, in the following form - (3)
  • Channel models like SCM, SCME, WINNER and IMT-Advanced are geometrical models comprising bi-directional clusters. Power azimuth spectra on transmitter and receiver ends are like in the example Figures 2 and 3.
  • clusters may be defined by the parameters described above. In other words, specular scatterers are not essential part of the model, they are just tools to generate channel coefficients.
  • the fading including Doppler and possible BS antenna correlation as well as channel power delay profile, is included in the channel coefficients. Only the DUT antenna correlation and other DUT antenna effects are left out to real radio transmission in the OTA chamber.
  • Doppler frequencies v n, m may be determined based on AoA angles.
  • H n (W) The result is a discrete impulse response with vector coefficients H n (W).
  • Dimensions of H n (t,t) are 1xS, where S is the number of BS antennas.
  • This step can be done by a Matlab implementation of a geometric channel model, e.g. NEWCOM model. Mapping of the clusters n may be performed to proper emulator channels and OTA antennas depending on the cluster nominal direction and the cluster angle spread.
  • An approximation of cluster arrival angle spread by two OTA antennas may be a source of inaccuracy.
  • Figure 2 illustrates a power azimuth spectrum of reception beams from five clusters.
  • the x-axis is angle in degrees and the y-axis is power in decibels.
  • the five beams 200, 202, 204, 206 and 208 are received at different angles of arrival.
  • the beams 200, 202, 204, 206 and 208 may be received at different moments of time i.e. at least one of them may have a different delay with respect to the other beams.
  • Figure 3 shows a power azimuth spectrum of transmission beams to the same five clusters according to the example in Figure 2.
  • the x- axis is angle in degrees and the y-axis is power in decibels.
  • the five beams 300, 302, 304, 306 and 308 are transmitted at only a slightly different angles of departure since the reflecting and/or scattering clusters are only slightly dispersed in the angle.
  • Figure 4 presents an OTA test chamber.
  • a DUT 400 is in the centre and chamber antenna elements 402, 404, 406, 408, 410, 412, 414 and 416 are in a circle around the DUT 400 with uniform spacing (e.g. 45° with 8 elements).
  • the test chamber may be an anechoic room.
  • a DUT 400 such as a subscriber terminal may be surrounded by antenna elements 402, 404, 406, 408, 410, 412, 414 and 416 which are coupled to an emulator 418 which may be, for example, EB (Elektrobit) Propsim® C8.
  • the emulator 418 may comprise a processor, a memory and a suitable computer program.
  • the separation angle A ⁇ may be the same or different for any two successive antenna elements 402 to 416.
  • the antenna elements 402 to 416 may be at the same or different distances from the DUT 400 and the antenna elements 402 to 416 may be placed only in a sector instead of a full angle or a full solid angle.
  • the DUT 400 may also have one or more elements in the antenna.
  • Communicating with the DUT 400 over the air enables testing an antenna design, polarization and placement effects in such a way that path directions may be freely included in the testing. That is not possible if a cable connection is used between the emulator 418 and the DUT 400.
  • the emulator 418 has a channel model for the test.
  • the channel model may be selected by a person accomplishing the test. Additionally, inter- ference and noise may be input to the test in a desirable manner and to a desirable extent.
  • the channel model used may be a play back model based on a recorded channel from a real radio system or it may be an artificially generated model or it may a combination of a play back model and an artificially generated model.
  • the emulator 418 is coupled to or acts as a base station of a radio system and the antenna elements 402 to 416 are transmitting to the DUT 400 which acts as a receiving subscriber terminal of the radio system. It may be assumed that DUT antenna characteristics are unknown and that information may be ignored in the following example.
  • the OTA antenna elements 402 to 416 may be assumed to be at angles 6k of directions from the DUT, where k is 1 , ... , K, where K is the number of antenna elements.
  • a geometric channel model in the emulator 418 may be mapped on the OTA antenna elements 402 to 416.
  • the emulator 418 simulates the situation where the transmitted radiation from the base station hits clusters.
  • the emulator 418 also forms a reflected and/or scattered beam from each cluster and divides the departure power and delay of the cluster suitably to the at least one antenna element 402 to 416.
  • the antenna elements 402 to 416 are controlled to reproduce reflected and/or scattered beams of clusters.
  • an angle of a beam representing a reflected and/or scattered beam from a cluster differs from an angle 6k of an antenna element 402 to 416 more than a threshold which may be, for example, 1°. Then such a beam may be transmitted using at least two antenna elements 402 to 416.
  • the power of a simulated cluster may be divided between two antenna elements on the basis of antenna angles 6k and a cluster angle ⁇ n .
  • An angle 6k of an antenna element k closest to a cluster angle ⁇ n may be found according to the following mathematical equation m j in r j + 2 A ⁇ " ⁇ n
  • min means minimum value of the expression among all values of 6j
  • int means an integer value of the division (including 0).
  • the value of k is
  • the selected antenna elements may be those between which the beam reflected and/or scattered from a cluster at least mainly is with respect to the DUT 400.
  • a selection of the OTA antennas for a cluster n can be done by selecting the two closest values of ⁇ k to AoA nominal angle ⁇ n .
  • the power of cluster n is divided between the two OTA antennas depending on angular distance between ⁇ k and ⁇ n . If e.g. ⁇ n is exactly on the middle between ⁇ k and ⁇ k +i the power is divided 50% and 50% for each.
  • a weight w ⁇ for each antenna element 402 to 416 may be calculated in the following manner
  • k is index of an antenna element closest to an angle ⁇ n of a cluster n.
  • Figure 10 presents an AoA in an OTA chamber.
  • a line 1000 is an AoA vector and circles are OTA antenna elements around the DUT 400.
  • Figure 11 presents antenna weighting of the antenna elements of Figure 10.
  • a curve 1100 depicts a beam of the antenna elements seen by a receiver.
  • Two weights 1102, 1104 of the antenna elements are non-zero while the rest are zero.
  • a power P k for antenna element 402 becomes O 0 - 37°
  • Figure 5 illustrates the beam 500 formed by the antenna elements 402, 404 with the calculated power division.
  • the signals fed to different antenna elements may also be phase shifted with respect to each other such that a directional power spectrum may be modified.
  • the phase shifting may be performed by weighting the base band signals with suitable complex coefficients which set powers and relative delays of the signals.
  • the phase shifting may also be performed by delaying the radio frequency signals with respect to each other. For example, desired delays may be selected suitably from a bank of digital delays (for example digital finite impulse response filter structure).
  • Different beams of different paths of the simulated radio channel may be formed at different moments of time.
  • a beam of a path of the simulated radio channel may be formed at different moments of time.
  • a plurality of different beams of different paths of the simulated radio channel may be formed at a moment of time.
  • Figure 6 presents a group 600 of antenna elements.
  • the antenna may comprise at least one group 600 of antenna elements 6002, 6004, 6006, 6008, 6010.
  • the antenna element 402 for example, there may not only be one antenna element but several elements 6002, 6004, 6006, 6008, 6010.
  • Each antenna element 402 to 416 may comprise, for example, five elements.
  • a mapping to OTA antenna elements may be simpler and more accurate if a single OTA antenna element is replaced by a group 600 of antenna elements 6002, 6004, 6006, 6008, 6010.
  • a group comprises G antenna elements 6002, 6004, 6006, 6008, 6010.
  • the number of elements 6002, 6004, 6006, 6008, 6010 to be fed in each antenna group 600 may be selected on the basis of a channel model arrival (per cluster) azimuth spread.
  • Each group may be fed by a single emulator output port, and antenna elements 6002, 6004, 6006, 6008, 6010 of each group may be connected to the emulator with a switching network 620 which may comprise at least one splitter, combiner, attenuator and/or phase shifter.
  • the switching i.e. selection of antenna elements
  • a beam controller 622 may control how many antenna elements of a group are needed for a beam. In general, any positive integer number of antenna elements up to the maximum may be used.
  • a mapping of the channel model to an OTA antenna may be performed by applying the following rules. Set each of the clusters to appropriate emulator channels and OTA antenna elements depending on a nominal direction of a cluster. Selection of the OTA antenna elements for a cluster n may be made by taking closest OTA antenna group centre & for a nominal AoA ⁇ n of a cluster. Select the number of antenna elements, for example Z', within a group by a switch 622.
  • Figure 7 presents a DUT 400 surrounded by groups 600 to 614 of antenna elements.
  • each group 600 to 614 has three antenna elements.
  • a beam 700 may be formed using a group 602. With eight groups and five elements in each group a full circle may be covered with uniformly located antenna elements. If a cluster is extremely wide requiring a very wide beam, for example wider than A ⁇ , the cluster may be mapped to more than one antenna group.
  • a beam 700 may be formed using groups 600 and 602.
  • fixed weights may be implemented for antenna elements such that, for example, Gaussian or Laplacian shaped cluster power azimuth spectrum can be replicated.
  • a reception using at least two antenna elements is performed in a corresponding manner.
  • the method may be applied in both uplink and downlink.
  • the antenna elements 402 to 416 are receiving signals from the DUT 400.
  • Signals received by the at least two antenna elements 402 to 416 may be combined in the emulator 418 for forming a reception beam of a signal of a path of a simulated radio channel.
  • the combining may comprise weighting the power from the two antenna elements or group of antenna elements using weights w n ⁇ +i calculated in equations (4) and (5).
  • the shape and direction of the beam may be weighted using complex coefficients or another sort of phase shifting.
  • the embodiments may be applied in 3GPP (Third Generation Partnership Project) LTE (Long Term Evolution), WiMAX (Worldwide Interoperability for Microwave Access), Wi-Fi and/or WCDMA (Wide-band Code Division Multiple Access).
  • MIMO Multiple In Multiple Out
  • FIG 8 shows a MIMO configuration having two transmit antenna elements 800, 802 and two receive antenna elements 804, 806. There are two delay taps 808, 810 representing different paths in delay elements 814 to 820 of an emulator 812. Signals from each transmit antennas 800, 802 are fed to delay elements 814 to 820 delaying the signals with the same delays (taps 808, 810).
  • delay elements 814 and 820 which delay with both delays (taps 808, 810) are combined and fed to the antenna element 806.
  • the outputs of delay ele- ments 816 and 818 which also delay with both delays (delay taps 808, 810) are combined and fed to the antenna element 804.
  • Figure 9 shows an example of a present embodiment. Also in this example there are two transmit antenna elements 900, 902 and two receive antenna elements 904, 906 of a plurality of antenna elements in an anechoic chamber 922 of the OTA test. There are two delay taps 908, 910 representing different paths in delay elements 914 to 920 of an emulator 912. A signal from a transmit antenna 900 is fed to delay elements 914, 916. The delay element 914 delays the signal with a delay corresponding to the delay tap 908 and the delay element 916 delays the signal with a delay corresponding to the delay tap 910. A signal from a transmit antenna 902 is fed to delay elements 918,
  • the delay element 918 delays the signal with a delay corresponding to the delay tap 910 and the delay element 920 delays the signal with a delay corresponding to the delay tap 908.
  • the outputs of delay elements 914 and 920 which delay with the same delay (delay tap 908) are combined and fed to the antenna element 906.
  • the outputs of delay elements 916 and 918 which delay with the same delay (delay tap 910) are combined and fed to the antenna element 904.
  • different delay taps are fed to different antenna elements 904, 906 if they represent a different AoA.
  • L ⁇ norm method For an accurate spatial correlation modelling, a cost function such as an lAnorm E p (g- ⁇ , g2,... , g «) may be optimized
  • p(A m , ⁇ Q ⁇ ⁇ ) is a theoretical spatial cross correlation on a separation ⁇ ⁇ m of antenna elements
  • ⁇ 0 is a nominal AoA
  • ⁇ ⁇ is an angular spread
  • ⁇ ( ⁇ m ) is a spatial correlation obtained with the OTA antenna elements.
  • the purpose is to determine weights g k of OTA antenna elements by minimizing the cost function above with respect to weights of the antenna elements.
  • the optimization may be performed by a gradient method, a half space method or the like.
  • K' 3, ⁇ k e ⁇ 0°, 45°, 90°, 135°, 180°, 225°, 270°, 315°, 360° ⁇ and g k may be limited such that g k e [0,1].
  • a practical value for ⁇ m is 0.6 and M about 50.
  • the eq. (8) can be computed by applying (9) and (10) and using numerical optimization methods, such as a gradient method and a half space method.
  • numerical optimization methods such as a gradient method and a half space method.
  • the equation is opened to more analytical form.
  • the weights in order to simplify the notation let us denote the weights as a vector
  • Equation (15) represent an analytical set of equations, i.e. making the gradient (14) as zero.
  • the nominal arrival angle ⁇ o in eq. (10) and (11) may be rounded to the closest OTA antenna element direc- tion ⁇ k .
  • K' OTA antenna elements an odd number of antennas
  • weight w n , ⁇ for a cluster n and an antenna element k may be written as
  • Figure 12 presents an example of a theoretical spatial correlation 1200 of three antenna elements and an ideal spatial correlation 1202 of 35° Laplacian PAS, 8 OTA antenna elements with 45° spacing.
  • the positions of antenna elements are fixed.
  • the directions between OTA antennas need to be interpolated. This can be done by minimizing the norm of eq. (6) by using the actual nominal arrival angles ⁇ o without any rounding.
  • Fig- ure 14 presents a theoretical spatial correlation 1400 of three antenna elements and ideal spatial correlation 1402.
  • the target AoA was 100° and the target cross correlation on 0.5 wavelength separation
  • 0.2476.
  • a resulting correlation matrix Rrx_abs is given below and the resulting maximum on PAS in Figure 4 a) is 101°.
  • the channel impulse responses are fed to the emulator and convolved with the transmitted signal.
  • the impulse responses of different MIMO channels have equal power delay profile and number of taps.
  • the modelling for the OTA environment is different.
  • the channel impulse responses may be disassembled and reassembled for different OTA antenna elements based on AoA information of clusters (taps).
  • the original PDP Power Delay Profile
  • the delay tap mapping of eight channels in the OTA emulation case is depicted in Figure 16. There are six clusters each having a different delay.
  • HZM w n,k H . Jt, ⁇ )exp(j2 ⁇ C k j), (19)
  • Figure 17 present a situation where a DUT spatial resolution is 24°, a number of OTA antenna elements is 8, a spacing of the antenna elements is 45°. The OTA antenna elements are marked with circles.
  • a reference number 1700 refers to AoA vector and a reference number 1702 refers to a velocity vector.
  • Figure 18 present a PAS 1800 seen by the receiver in the situation described in Figure 17. Circles 1802 depict a relative power of the antenna elements.
  • the PAS 1800 has two peaks and that is not desirable.
  • Figure 19 present a situation where a DUT spatial resolution is 24°, the number of OTA antenna elements is 16, spacing of the antenna elements is 22.5°.
  • the OTA antenna elements are marked with circles.
  • a reference number 1900 refers to AoA vector and a reference number 1902 refers to a velocity vector.
  • Figure 20 present a PAS 2000 seen by the receiver in the situation described in Figure 19.
  • Circles 2002 depict a relative power of the antenna elements.
  • the PAS 2000 has only one peak and that is desirable.
  • the DUT antenna array size determines the spatial resolution.
  • a rule of thumb resolution for I/2 ULA is 96 7#DUT antennas. For example, a two antenna ULA results in 48° AoA and a 4 antenna ULA results in 24° AoA.
  • a spacing between OTA antenna elements is desirably smaller than a spatial resolution of the DUT.
  • the fading including Doppler and possible correlation of antenna elements of OTA as well as channel power delay profile, may be included in the channel coefficients.
  • Channel coefficients may be generated by a modified version of eq.
  • the channel coefficient formula may be written separately for V and H polarizations:
  • F ⁇ x and F" x are field patterns of V (Vertical) and H (Horizontal) polarizations of the antenna elements, respectively.
  • Phase terms ⁇ n v ⁇ , etc. are random initial phases e [0,2 ⁇ J and ⁇ n m are cross polarization power ratios (XPR).
  • Doppler frequencies v n , m are still determined on the basis of AoA angles.
  • the result is a discrete impulse response with matrix coefficients H n (t, ⁇ ).
  • Dimensions of H n (t, ⁇ ) are in single polarized case 1 x S and in dual polarized case 2 x S, where S is the number of OTA antenna elements.
  • This step can be done by a Matlab implementation of a geometric channel model, e.g. SCME or WINNER model.
  • mapping of the clusters n to proper emulator channels and OTA antenna elements depending on a cluster nominal direction and a cluster angle spread may be performed.
  • the selected method may depend on whether accurate AoA (referring to eq. (5)), accurate spatial correlation (referring to eq. (16)) or balanced combination of the both (referring to Figure 14 and its explanation) is emphasized.
  • the methods are described for a single polarized case, but they are applicable also in the dual polarized case. The only difference is that in a dual polarized case V (Vertical) and H (Horizontal) polarized channel impulse responses from eq. (21) and (22) may be mapped separately to V and H polarized OTA antenna elements.
  • Figure 22 presents an OTA chamber antenna setup with eight uniformly spaced dual polarized chamber antenna elements 2202, 2204, 2206, 2208, 2210, 2212, 2214 and 2216.
  • the V-polarized elements are actually orthogonal to the paper (azimuth plane).
  • Figure 23 presents a flow chart of the method.
  • a cost function of a theoretical spatial cross correlation and a spatial correlation obtained with antenna elements is optimized for determining weights of the an- tenna elements.
  • a beam of a signal of at least one path of a simulated radio channel is formed with at least two antenna elements of a plurality of the antenna elements coupled to an emulator in an anechoic chamber.
  • Figure 24 presents a flow chart of the method.
  • a cost function of a theoretical spatial cross correlation and a spatial correlation obtained with antenna elements is optimized for determining weights of the antenna elements.
  • the embodiments may be implemented, for instance, with ASIC or VLSI circuits (Application Specific Integrated Circuit, Very Large Scale Integration).
  • the embodiments of method steps may be implemented as a computer program comprising instructions for executing a computer process for communicating with an electronic device under test through a simulated radio channel of an emulator.
  • the emulator may control on the basis of the electronic circuits and/or the computer program the use of the antenna elements and the formation of beams in the anechoic chamber.
  • the computer program may be stored on a computer program dis- tribution medium readable by a computer or a processor.
  • the computer program medium may be, for example but not limited to, an electric, magnetic, optical, infrared or semiconductor system, device or transmission medium.
  • the computer program medium may include at least one of the following media: a computer readable medium, a program storage medium, a record medium, a computer readable memory, a random access memory, an erasable programmable read-only memory, a computer readable software distribution package, a computer readable signal, a computer readable telecommunications signal, computer readable printed matter, and a computer readable compressed software package.

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Spectroscopy & Molecular Physics (AREA)
  • General Physics & Mathematics (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Radio Transmission System (AREA)
  • Monitoring And Testing Of Transmission In General (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Aerials With Secondary Devices (AREA)
  • Testing Electric Properties And Detecting Electric Faults (AREA)

Abstract

Système de test conçu pour optimiser une fonction de coût d’une corrélation spatiale croisée théorique et d’une corrélation spatiale obtenue au moyen d’éléments d’antenne (402 à 416) en vue d’établir des facteurs de pondération des éléments d’antenne (402 à 416), et pour former un faisceau d’un signal d’au moins un trajet d’un canal radioélectrique simulé, au moins deux éléments d’antenne (402 à 416) d’une pluralité d’éléments d’antenne (402 à 416) étant reliés à un émulateur (418) dans une chambre anéchoïque. Lesdits au moins deux éléments d’antenne sont capables de polariser le faisceau d’une manière connue.
EP09818841.0A 2008-10-06 2009-02-25 Test par voie aérienne Active EP2347531B1 (fr)

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PCT/FI2008/050554 WO2010040887A1 (fr) 2008-10-06 2008-10-06 Test par voie hertzienne
PCT/FI2009/050155 WO2010040889A1 (fr) 2008-10-06 2009-02-25 Test par voie aérienne

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KR20110087281A (ko) 2011-08-02
US20110191090A1 (en) 2011-08-04
TWI434527B (zh) 2014-04-11
WO2010040887A1 (fr) 2010-04-15
US11152717B2 (en) 2021-10-19
JP5280544B2 (ja) 2013-09-04
CA2738111A1 (fr) 2010-04-15
EP2347531B1 (fr) 2013-09-18
TWI453675B (zh) 2014-09-21
US20110189962A1 (en) 2011-08-04
TW201015442A (en) 2010-04-16
JP2012504887A (ja) 2012-02-23
JP2012504886A (ja) 2012-02-23
TW201015885A (en) 2010-04-16
KR101308212B1 (ko) 2013-09-13
WO2010040889A1 (fr) 2010-04-15
US9786999B2 (en) 2017-10-10
KR101328760B1 (ko) 2013-11-13
CA2739042A1 (fr) 2010-04-15
KR20110087279A (ko) 2011-08-02
EP2345183A1 (fr) 2011-07-20
EP2347531A4 (fr) 2012-10-10
EP2345183A4 (fr) 2013-11-06

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